BACKGROUND OF THE INVENTION
[0001] There are multiple automotive, marine and aviation applications where small, low
cost millimeterwave (MMW) radar sensors are distributed around a vehicle to provide
functions, such as adaptive cruise control, anti-collision warning, brake applications,
parking, marine threat detection or marine docking guidance.
[0002] Many developers have created low cost MMW sensors, particularly for the automotive
marketplace where production numbers can be in the 100,000s. Most use modulation that
is either FM/CW or UltraWideband. In the typical application, each sensor provides
its own modulation and signal processing in a single package. Adding more sensors
requires adding complete radar and signal processing/control systems to each location
and then combining data from each in yet another computing platform. This duplicates
many functions.
[0003] The RF implementation of the MMW Radar subsystems has either been overly complex
(frequency multiplication systems) or overly simple with poor RF performance (MMW
Oscillator directly connected to an antenna and modulated). Both systems generate
very high phase noise and varying modulation characteristics over time and environmental
changes.
[0004] U.S. patent 7,324,039 to Boltovets et al. attempts to generate a MMW radar signal by frequency multiplication of an open loop
X band Voltage Controlled Oscillator. This choice for FM/CW modulation also directly
multiplies any modulation non-linearity and causes phase noise to increase by a factor
of 20 Log N where N is the multiplication factor. Both factors significantly degrade
the performance of the resulting system.
[0005] Overly simple systems that employ a directly modulated MMW VCO to avoid the use of
frequency multiplication achieve an overly sensitive VCO that is easily made non-linear
by circuit effects, temperature or movement of objects present in the antenna beam.
SUMMARY OF THE INVENTION
[0006] The present invention provides a low cost means to achieve the needed sensitivity
of the microwave or MMW radar sensors with low phase noise and accurate modulation
at the lowest possible cost of signal generation and signal processing. The proposed
system has the advantage being scaled in size from one sensor to many sensors, all
served by a common control and signal processing system.
[0007] An example radar system includes a processor and a plurality of transceivers having
antenna(e). The transceivers and/or antennas of the transceivers are located at various
points around the vehicle. The transceivers include receive and transmit electronics
that are in signal communication with the corresponding antenna for outputting radar
signals. The transmit electronics include a voltage controlled oscillator (VCO), a
dielectric resonator oscillator (DRO), a phase locked loop (PLL) component and a direct
digital synthesizer (DDS). The receive electronics receive from the antenna any radar
reflections corresponding to the outputted radar signals and send signals associated
with the radar reflections to the processor. The processor generates output signals
based on the signals received from the plurality of transceivers.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Preferred and alternative embodiments of the present invention are described in detail
below with reference to the following drawings:
[0009] FIGURE 1 is a block diagram of a system implemented on a vehicle or a building;
[0010] FIGURES 2 and 3 are system diagrams of example transceivers formed in accordance
with embodiments of the present invention; and
[0011] FIGURES 4-6 illustrate the systems of FIGURE 1 implemented on various vehicles.
DETAILED DESCRIPTION OF THE INVENTION
[0012] As shown in FIGURE 1, the present invention provides a system 20 that includes a
master signal processor 22 in signal communication with one or more radar components
24. The radar components 24 translate an operating frequency to Microwave or millimeterwave
(MMW) range by mixing it with an "open loop" oscillator that operates at MMW frequencies
that offers frequency stability over time, temperature and vibration, such as a Dielectric
Resonator Oscillator (DRO) (example DROs are produced by Honeywell Inc.). The DRO
provides excellent frequency stability over time, temperature and load conditions
with very low phase noise. An array of radar components 24 are mounted to a vehicle
or building and are controlled by the processor 22. The processor 22 determines if
any of the radar components 24 have sensed any objects and outputs that determination
to an operator.
[0013] The processor 22 provides control signals for altering the modulation or antenna
scanning at each radar component 24. The processor 22 is programmable such that a
sequence of modulation rates can be applied to the radar components 24 so that each
is optimized for its application and location on a vehicle. The results measured by
adjacent radar components 24 can be directly compared to generate additional intelligence
about the dangers or situation around the vehicle.
The processor 22 permits the coordination of the multiple sensors (the radar components
24) - causing them to be synchronous and have specific offset frequencies in order
to prevent jamming /interfering with each other. The processor 22 also has the ability
to "sweep" from sensor to sensor to collect an overall image/data of the surroundings
by interrogating them sequentially. This permits a single DSP/signal processing capability
to be reused multiple times, thereby producing the unexpected results of reduced cost,
power consumption, volume and weight. The processor 22 can also dwell at one sensor
(the radar components 24) for as long as needed or jump between sensors as required
as well with no particular pattern, according to the surveillance needs.
[0014] As shown in FIGURE 2, an example radar component 24-1 includes a suitable microwave
or MMW voltage controlled oscillator (VCO) 40 and a DRO 42 that is tuned to a frequency
at a predefined level below the lowest expected VCO frequency. The output of the VCO
and the DRO are mixed at a mixer 48 to generate an intermediate (IF) that may be divided
down to produce an input signal to a phase locked loop (PLL) chip 50, such as that
produced the ADF 4111 PLL manufactured by Analog Devices. The PLL chip 50 provides
some frequency division and a Phase/Frequency detector and a charge pump are used
to close the PLL chip 50. The PLL chip 50 includes the charge pump, phase/freq detector
and frequency division component. The PLL chip 50 provides desired linearity and low
phase noise present in both the DRO and VCO of approximately (-100dBc/Hz at 100 KHz).
[0015] In one embodiment, as shown in FIGURE 2, the radar component 24-1 is a dual antenna
transceiver. As shown in FIGURE 3, a radar component 24-2 is a single antenna transceiver.
The receiver and transmitter components within the radar components 24-1 and 24-2
are the same except that the single antenna transceiver includes a circulator device
attached to the antenna. A direct digital synthesizer (DDS) 52 provides a reference
input signal to the PLL chip 50 based on signal from a clock 54. In one example, the
clock 54 is a 125 MHz clock that causes the DDS 52 to produce the reference input
signal at 25-31.25 MHz. The DDS frequencies are independent of the VCO and of the
MMW operating frequency. The output of the PLL chip 50 is amplified and filtered then
input to the VCO 40. The VCO 40 generates a signal that is amplified, filtered by
a band pass filter, sent to the mixer 48 and then sent to a transmit antenna and receive
antenna mixer via couplers.
[0016] The RF input to the mixer 48 is a sample of the entire transmitted bandwidth of the
MMW sensor. So for example, if the sensor transmits between 24.00 GHz and 24.20 GHz
(200 MHz BW) then the input to 48 RF port is 24.00 to 24.20 GHz. The exact bandwidth
depends on the frequency division and the programmed frequency division within the
PLL chip itself. So this system is programmable for many frequency ranges.
[0017] For a 24 GHz Radar that has FM/CW modulation between 24.00 and 24.20 GHz select a
VCO that tunes from F (24.00GHz) to F+0.2 GHz (24.2GHz). Then one chooses a DRO at
F-0.8 (23.2 GHz). When the DRO frequency is mixed with the VCO frequency range between
24 and 24.2 GHz the difference of the two frequencies is 0.8 to 1.0 GHz. Those difference
frequencies of 0.8 to 1.0 GHz are the input to the PLL where it is divided by 32 within
the PLL chip (e.g., ADF 4111) to produce 25 - 31.25 MHz that is in turn compared to
the DDS input over the same frequency range. The use of the DRO to create a modest
IF frequency range near 1 GHz is critical to permitting very low frequency divider
ratios or the elimination of frequency multiplication modules. The DRO preserves very
low phase noise that would otherwise be substantially higher with other methods.
[0018] If a wider bandwidth is desired, it is easy to increase the DDS bandwidth from 6.25
MHz to 12.5 MHz. The DDS chirp bandwidth is multiplied by the PLL via the divider
ratio. So if the divide ratio is 32 and the DDS chirps over 12.5 MHz then 32 x 25
= 400 MHz of Chirp bandwidth with no change in phase noise performance from the 200
MHz chirp bandwidth. In this case the IF frequency range at the input to the PLL chip
(ADF 4111) would increase from the original 0.8 to 1.0 GHz to 0.8 to 1,2 GHz. This
IF frequency range will track the actual bandwidth of the modulated millimeter wave
frequency source.
[0019] In one embodiment, carbon fiber composites enclose each of the radar components 24
to provide exceptionally strong and EMI/EMC absorption that prevents the radar components
24 from jamming or being jammed by other sensors on other vehicles etc. and at the
same time provides physical protection from an outdoor environment.
[0020] A receive side of the radar components 24-1 and 24-2 includes common radar receiver
components. The received signals are converted to digital then sent to the master
processor 22 for analysis. Communication between the components 24-1 and 24-2 can
be done over a data bus, fiber optic coils, wirelessly or by any other comparable
means.
[0021] The sensors operate in the same band (i.e., 24 GHz, 77 GHz, 35 GHz, 95 GHz) but not
at the same exact frequency ranges. Because the master controller 22 can command the
sensors 24 it can do two things: 1) command specific frequency ranges for the FM/CW
modulation that is offset in frequency from any other sensor 24 by at least 1 to 2
times the IF frequency of the receiver (receiver mixer output); 2) it can synchronize
the start and stop times of the sensors to be exact so that the programmed frequency
difference between the sensors is always maintained throughout the frequency modulation
period. That exactly prevents jamming or interaction among the sensors.
[0022] FIGURE 4 illustrates a top, partial view of a ship having four radar components 24
mounted on exterior surfaces of the ship and the master processor 22 being located
to receive data from the radar components 24. FIGURES 5 and 6 illustrate similar systems
mounted on a car and an aircraft.
In one embodiment, the system 20 is adaptable to any legal radar band up to 95 GHz
with a common digitally synthesized control loop. It can go higher than 95 GHz. There
is no fundamental limitation at 95GHz except that most typical operating bands end
there. When you get to 100 GHz and above you get close to bands known as "Near IR"
- meaning that you are approaching the wavelengths of Infrared radiation.
1. A radar system located on a vehicle, the system comprising:
a central processor (22);
a plurality of sensor transceivers (24) located at various points around the vehicle,
the plurality of sensor transceivers being in signal communication with the central
processor, the plurality of sensor transceivers comprising:
at least one antenna (24);
receive electronics in signal communication with the at least one antenna and the
processor; and
transmit electronics in signal communication with the at least one antenna, the transmit
electronics configured to output radar signals via the at least one antenna, the transmit
electronics comprising:
a voltage controlled oscillator (VCO) (40);
a dielectric resonator oscillator (DRO) (42);
a phase locked loop (PLL) component (50); and
a direct digital synthesizer (DDS) (52),
wherein the receive electronics are configured to receive from the at least one antenna
any radar reflections corresponding to the outputted radar signals and to send signals
associated with the radar reflections to the processor,
wherein the central processor is configured to generate output signals based on the
signals received from the plurality of sensor transceivers.
2. The system of Claim 1, wherein the transmit electronics further comprises:
a mixer configured to combine a signal produced by the DRO with a signal produced
by the VCO; and
components configured to divide the output of the mixer and producing an input signal
to the PLL component,
wherein the DDS produces a reference signal for the PLL component and the PLL component
generates a control signal for the VCO.
3. The system of Claim 2, wherein the transmit electronics further comprises a clock
configured to generate an input into the DDS.
4. The system of Claim 2, wherein the central processor is configured to coordinate the
plurality of sensor transceivers causing the plurality of sensor transceivers to be
synchronous and have specific offset frequencies in order to prevent one of jamming
or interfering with each other.
5. The system of Claim 2, wherein the central processor is configured to sweep from sensor
transceiver to sensor transceiver to collect data and generate a sense of surroundings
of the vehicle, to dwell at one of the sensor transceivers based on one of a predefined
protocol or manual request or to jump between the sensor transceivers based on one
of a predefined protocol or manual request.
6. A method for sensing targets located around a vehicle, the method comprising:
at each of a plurality of sensor transceivers:
transmitting radar signals via at least one antenna, transmitting comprising:
mixing a signal produced by a dielectric resonator oscillator (DRO) with a signal
produced by a voltage controlled oscillator (VCO);
dividing the output of the mixer to produce an input signal to a phase locked loop
(PLL) component; and
applying a reference signal produced by a direct digital synthesizer (DDS);
receiving from the at least one antenna any radar reflections corresponding to the
transmitted radar signals;
sending signals associated with the received radar reflections to a central processor;
and
generating at the central processor output signals based on the sent signals.
7. The method of Claim 6, wherein applying the reference signal comprises applying a
clock signal to the DDS.
8. The method of Claim 6, further comprising coordinating at the central processor the
plurality of sensor transceivers causing the plurality of sensor transceivers to be
synchronous and have specific offset frequencies in order to prevent one of jamming
or interfering with each other.
9. The method of Claim 6, further comprising sweeping the central processor to receive
from one sensor transceiver to another sensor transceiver to collect data and generate
information related to a sense of surroundings of the vehicle.
10. The method of Claim 6, further comprising dwelling the central processor at one of
the sensor transceivers based on one of a predefined protocol or manual request or
jumping the central processor between the sensor transceivers based on one of a predefined
protocol or manual request.